JPS6161909A - Air blower in radiator for water-cooled internal combustion engine - Google Patents

Air blower in radiator for water-cooled internal combustion engine

Info

Publication number
JPS6161909A
JPS6161909A JP60181956A JP18195685A JPS6161909A JP S6161909 A JPS6161909 A JP S6161909A JP 60181956 A JP60181956 A JP 60181956A JP 18195685 A JP18195685 A JP 18195685A JP S6161909 A JPS6161909 A JP S6161909A
Authority
JP
Japan
Prior art keywords
blower
blade
shroud
slit
impeller
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP60181956A
Other languages
Japanese (ja)
Other versions
JPH0240853B2 (en
Inventor
マンフレート・ノンネンマン
クルト・ハウゼル
ハンス‐デイーテル・ゴール
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Daimler Benz AG
Mahle Behr GmbH and Co KG
Original Assignee
Daimler Benz AG
Behr GmbH and Co KG
Mahle Behr GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Daimler Benz AG, Behr GmbH and Co KG, Mahle Behr GmbH and Co KG filed Critical Daimler Benz AG
Publication of JPS6161909A publication Critical patent/JPS6161909A/en
Publication of JPH0240853B2 publication Critical patent/JPH0240853B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • F01P5/04Pump-driving arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B67/00Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for
    • F02B67/04Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for of mechanically-driven auxiliary apparatus
    • F02B67/06Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for of mechanically-driven auxiliary apparatus driven by means of chains, belts, or like endless members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/326Rotors specially for elastic fluids for axial flow pumps for axial flow fans comprising a rotating shroud

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 ′ 〔産業上の利用分野〕 本発明は、送風機羽根車が送風機羽根車軸を介して内燃
機関に支持され、この送風機羽根車軸上に駆動ベルト用
ベルト車が設けられ、送風機羽根車が送風機羽イ1(の
外端を囲む取巻き送風機囲い板を備えている、水冷内燃
機関放熱器にある送風装置に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention provides a blower impeller supported by an internal combustion engine via a blower impeller shaft, and a driving belt pulley provided on the blower impeller shaft. The present invention relates to a blower device in a water-cooled internal combustion engine radiator, in which the blower impeller is provided with a surrounding blower shroud surrounding the outer end of the blower blades 1.

r従来の技術〕 送風機羽根車にある送風機羽根を囲んて羽根先端に取付
けられる送風機囲い板をもつこのような送風装置は、ド
イツ連邦共和国特許出願公開第2826697号明細書
から公知である。送風機羽根車は送風機羽根車軸を介し
て内燃機関に支持され、内燃機関から送風機羽根車およ
び別の補助機器を駆動する1つまたは複数のVベルトを
かけるシベルト車が、この送ノ!ti1機羽PM車軸上
に設けられている。
BACKGROUND OF THE INVENTION Such a blower device having a blower shroud which surrounds the blower blades of the blower impeller and is attached to the blade tips is known from DE 28 26 697 A1. The blower impeller is supported by the internal combustion engine via the blower impeller axle, and a Sibelt wheel that runs one or more V-belts driving the blower impeller and other auxiliary equipment from the internal combustion engine drives this blower impeller. The ti1 plane is installed on the PM axle.

さて取巻き送風機囲い板をもつ送風機羽根車では、欠陥
のあるVベルトの交換は、Vベルトの長さに応してかな
りの困難を伴う。例えば送風機囲い板の直径より大きい
直径をもつこのようなVベルトのみが、送風機羽根車を
越えて取付けまたは取外しのためこれを単にすらすこと
によって、容易に交換される。これに反し送風機囲い板
の直径より小さい直径をもつVベルトは、送風機羽根車
全体を取外した後にのみ交換され、これにはかなりの時
間と費用を伴う。
Now, in blower impellers with surrounding blower shrouds, replacing a defective V-belt involves considerable difficulty depending on the length of the V-belt. Only such a V-belt, for example with a diameter larger than that of the blower shroud, is easily replaced by simply sliding it past the blower impeller for installation or removal. In contrast, a V-belt with a diameter smaller than that of the blower shroud is replaced only after the entire blower impeller has been removed, which involves considerable time and expense.

〔発明が解決しようとする間Na〕[Na while the invention is trying to solve]

さて本発明の基礎になっている課題は、最初にあげた送
風装置を改良して、送風機囲い板の直径より小さい直径
をもつベルトも送風機羽根車の取外しなしに交換できる
ようにすることである。
The problem on which the present invention is based is to improve the blower device mentioned at the beginning so that belts with a diameter smaller than the diameter of the blower shroud can also be replaced without removing the blower impeller. .

〔問題点を解決するための手段〕[Means for solving problems]

このWAfRを解決するため本発明によれば、送風機囲
い板が、ベルトを入れて送風機羽根車の軸のない端面に
あるベルト部分を送風機囲い板を越えてすらすための少
なくとも1つの軸線方向に延びるスリッ1〜をもってい
る。
In order to solve this WAfR, the present invention provides that the blower shroud is arranged in at least one axial direction for receiving the belt and allowing the portion of the belt at the non-axial end face of the blower impeller to slide past the blower shroud. It has an extending slit 1.

本発明により、羽根に固定した取巻き送風機囲い板をも
つ送風機でも、送風機羽根車を取外すことなく欠陥のあ
るベルトを交換することができる。
The present invention allows defective belts to be replaced without removing the blower impeller, even in blowers with wraparound blower shrouds fixed to the blades.

本発明のそれ以外の構成が特許請求の範囲の従属用の対
象である。
Other embodiments of the invention are subject to dependent claims.

〔実施例〕〔Example〕

図面には本発明の異なる実施例が示されている。 The drawings show different embodiments of the invention.

第1図には、水冷内燃機関の放熱器用送風装置のうち送
風機羽根車1だけが示されている。
In FIG. 1, only a blower impeller 1 of a blower device for a radiator of a water-cooled internal combustion engine is shown.

送風機羽根車lは送風機ボス2をもち、半径方向に突出
する送風機羽根3がこの送風機ボス上に取付けられてい
る。送風機羽根3は、羽根先端5で送風機羽根3に結合
される送風機囲い板4により囲まれている。第1図には
、送風機羽根車1が下流側に取付けられる送風機羽根車
軸を介して内燃機関の端面に回転可能に支持されている
ことは示してない。送風機羽根車軸上にはVベルト6用
の■ベルト車が取付けられ、このVベル)−を介して送
風機羽根車1がクランク軸から駆動される。別のVベル
トを介して、内燃機関に設けられた補助機器を送風機羽
根車軸から同時に駆動することができる。
The blower impeller l has a blower boss 2 on which radially projecting blower blades 3 are mounted. The blower blades 3 are surrounded by a blower shroud 4 which is connected to the blower blades 3 at the blade tips 5. It is not shown in FIG. 1 that the blower impeller 1 is rotatably supported on the end face of the internal combustion engine via a downstream-mounted blower impeller axle. A belt pulley for the V-belt 6 is mounted on the blower impeller shaft, and the blower impeller 1 is driven from the crankshaft via this V-belt. Via a further V-belt, auxiliary equipment on the internal combustion engine can be simultaneously driven from the blower blade axle.

内燃機関において望まれるこじんまりした構造のため、
Vベルトは全長が比較的短く、その結果送風機囲い板4
の直径より通常は小さい直径をもっている。
Due to the compact structure desired in internal combustion engines,
The V-belt has a relatively short overall length, and as a result, the blower shroud 4
It usually has a smaller diameter than the diameter of the

送風機羽根車1を取外すことなくこのようなVベルトを
取付けることができるようにするため、送風機囲い板4
は軸線方向に延びるスリット7を備えている。第1図に
よれば、スリット7は2つの送風機羽根3の間に延びる
送風機囲い板4の周範囲にある。■ヘルド6は取付けの
ため外からスリット7を通して2つの送風機羽根3の間
へ挿入されて、送風機ボス2の所まで押しやられる。そ
の際スリット7が送風機羽根車lの上側にあると、■ベ
ルト6は続いて送風機羽根車の下側へ実線で示す位置へ
落下する。
In order to be able to install such a V-belt without removing the blower impeller 1, the blower shroud 4
is provided with a slit 7 extending in the axial direction. According to FIG. 1, the slit 7 is located in the circumferential area of the fan shroud 4, which extends between the two fan blades 3. - For installation, the heald 6 is inserted from the outside through the slit 7 between the two blower blades 3 and pushed to the blower boss 2. At this time, when the slit 7 is located above the blower impeller l, the belt 6 subsequently falls to the position shown by the solid line below the blower impeller.

それから送風機羽根車1の軸のない端面の前にあるベル
ト部分8は、鎖線で示すように、送風機囲い板4の周囲
を越えて引張られる。今や■ベルト6は送風機羽根車軸
上に川・かり、■ベルト車上へ張りさえすればよい。
The belt section 8 in front of the shaftless end face of the blower impeller 1 is then pulled over the circumference of the blower shroud 4, as shown by the dashed line. Now, it is only necessary to place the belt 6 on the blower impeller axle and stretch it on the belt wheel.

送風機囲い板4の中断によりその強度がかなり低下する
。この強度低下を補償できるようにするため、第2図に
よれば、スリット7の両側にある囲い板片が、支柱とし
て構成されたそれぞれ1つの補助羽根】1および12を
介して送風機ボスに結合されている。スリット7のすぐ
そばに設けられる補助羽根11および12は別の形状を
もっていてもよい。しかし送風機羽根車1の効率を悪化
しない支柱のこのような形状が好ましい。
The interruption of the blower shroud 4 considerably reduces its strength. In order to be able to compensate for this loss of strength, according to FIG. 2, the shrouding plate pieces on both sides of the slot 7 are connected to the blower boss via one auxiliary vane 1 and 12, each configured as a support. has been done. The auxiliary vanes 11 and 12 provided in the immediate vicinity of the slit 7 may have other shapes. However, such a shape of the strut is preferred as it does not impair the efficiency of the blower impeller 1.

これとは無関係に、第2図に鎖線で示すように、スリッ
ト7を送風機羽根3のすぐ近くに設けて、例えばスリッ
ト7の左側の囲い板片を直接送風機羽根3を介して支え
、囲い板片9を特別な補助羽根11を介して支祁えすれ
ばよいようにもすることがてきる。これにより補助羽根
12を省略することができる。
Irrespective of this, as shown by the chain line in FIG. 2, the slit 7 is provided in the immediate vicinity of the blower blade 3, and, for example, the shroud plate piece on the left side of the slit 7 is directly supported via the blower blade 3, and the shroud It is also possible to support the piece 9 through special auxiliary blades 11. This allows the auxiliary blade 12 to be omitted.

第3図の実施例では、スリット7が送風機羽根3の半径
方向延長部に延びる囲い板部分13に設けられている。
In the embodiment of FIG. 3, the slit 7 is provided in a shroud portion 13 extending in the radial extension of the blower blade 3. In the embodiment of FIG.

送風機羽根3は切欠き14をもち、スリット7はこの切
欠き14を通って送風機ボス2の範囲まで続いている。
The blower blade 3 has a cutout 14 through which the slit 7 continues in the area of the blower boss 2.

これによりスリットの両側にある両囲い板片15および
16の補強結合のための2つの支柱を省略することがで
きる。
This makes it possible to dispense with two supports for the reinforcing connection of the two shroud plates 15 and 16 on both sides of the slit.

第4図の実施例では、送風機囲い板の囲い板部分17に
おいて、送風機羽根19と20との間にスリット18が
設けられている。スリツh18は送風機羽根の軸線方向
経過および輪郭に従って弧状に構成されている。スリッ
トにより囲い板部分17内に形成される縦縁21および
22は、それぞれ送風機羽根1つおよび20の互いに向
き合う羽根面23および24の半径面内にある。縦縁2
1は送風機羽根19の羽根面23の経過に従い、縦縁2
2は補助羽根20の羽根面24の経過に従う。これによ
りスリット18の全軸線方向区間にわたって、支柱とし
ての羽根19および20が縦縁21および22に及ぶよ
うにすることができる。
In the embodiment of FIG. 4, a slit 18 is provided between the blower blades 19 and 20 in the shroud portion 17 of the blower shroud. The slots h18 are arc-shaped in accordance with the axial course and contour of the blower blades. The longitudinal edges 21 and 22 formed by the slits in the shroud part 17 lie in the radial plane of the mutually facing vane surfaces 23 and 24 of the blower blades 1 and 20, respectively. Vertical edge 2
1 follows the progress of the blade surface 23 of the blower blade 19, and the vertical edge 2
2 follows the course of the blade surface 24 of the auxiliary blade 20. This allows the blades 19 and 20 as struts to extend over the longitudinal edges 21 and 22 over the entire axial section of the slot 18.

本発明の範囲内において、送風機囲い板4に取付けられ
るキャップによりスリット7または18を覆うことも考
えられる。さらに金属板またはプラスチック構成の取巻
き送風機囲い板をもつ軸流送風機や半軸流送風機にも、
本発明による手段の適用が可能である。最後に、提案さ
れた手段は、内燃機関のクランク軸から直接駆動される
ような送風機羽根車にも適用可能である。
It is also conceivable within the scope of the invention for the slit 7 or 18 to be covered by a cap that is attached to the blower shroud 4 . Furthermore, axial and semi-axial fans with surrounding fan shrouds of metal plate or plastic construction are also available.
It is possible to apply the measures according to the invention. Finally, the proposed measures are also applicable to blower impellers that are driven directly from the crankshaft of an internal combustion engine.

その際送風機羽根車軸上に設けられる■ベルト車は、補
助駆動装置または補助機器の駆動のみに用いられる。
In this case, the belt pulley provided on the blower impeller shaft is used only for driving the auxiliary drive device or auxiliary equipment.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は取巻き送風機囲い板をもつ送風機羽根車の正面
図、第2図は送風機囲い板にある本発明によるスリット
の平面図、第3図は送風機羽根の半径面にスリッl〜を
設けられた送風機囲い板の一部の平面図、第4図は送風
機羽根の輪郭および経過にスリットを合わせた送風機囲
い板の一部の平面図である。 1・・・送風機羽根車、3・・・送風機羽根、4・・・
送風機囲い板、6・・・ベルト、7.18・・・スリッ
ト。 特許出願人  ダイムラー−ベンツ・アクチェンゲゼル
シャフト ベール・ゲゼルシャフト・ミツト・ ベシュレンクテル・ハフラング・ ラント・コンパニ・コマンディート ゲゼルシャフト
FIG. 1 is a front view of a blower impeller with a surrounding blower shroud, FIG. 2 is a plan view of the slit according to the invention in the blower shroud, and FIG. FIG. 4 is a plan view of a portion of the blower shroud in which the slits are aligned with the contour and course of the blower blades. 1...Blower impeller, 3...Blower blade, 4...
Blower enclosure plate, 6...belt, 7.18...slit. Patent applicant Daimler-Benz Akchengesellschaftbeer Gesellschaft Mitsut Beschrenktel Hafrang Land Kompani Kommandiet Gesellschaft

Claims (1)

【特許請求の範囲】 1 送風機羽根車が送風機羽根車軸を介して内燃機関に
支持され、この送風機羽根車軸上に駆動ベルト用ベルト
車が設けられ、送風機羽根車が送風機羽根の外端を囲む
取巻き送風機囲い板を備えているものにおいて、送風機
囲い板(4)が、ベルト(6)を入れて送風機羽根車(
1)の軸のない端面にあるベルト部分を送風機囲い板(
4)を越えてずらすための少なくとも1つの軸線方向に
延びるスリット(7、18)をもつていることを特徴と
する、水冷内燃機関用放熱器にある送風装置。 2 スリット(7)が2つの隣接する送風機羽根(3)
の間にある送風機囲い板(4)の範囲に設けられ、スリ
ット(7)の両側にある囲い板片(9、10)が、それ
ぞれ支柱(11、12)を介して送風機ボス(2)に保
持されていることを特徴とする、特許請求の範囲第1項
に記載の送風装置。 3 支柱が補助羽根(11、12)として構成されてい
ることを特徴とする、特許請求の範囲第2項に記載の送
風装置。 4 一方の支柱が送風機羽根(3)により形成され、他
方の支柱が補助羽根(11または12)により形成され
ていることを特徴とする、特許請求の範囲第2項に記載
の送風装置。 5 スリット(7)が送風機羽根(3)の半径方向延長
部に延びる送風機囲い板(4)の囲い板部分(13)に
設けられて、送風機羽根(3)にある切欠き(14)を
通つて送風機ボス(2)の範囲まで続いていることを特
徴とする、特許請求の範囲第1項に記載の送風装置。 6 スリット(18)が送風機羽根(19、20)の輪
郭の軸線方向経過に従つて構成され、このスリットの両
縦縁(21、22)が隣接する送風機羽根(19、20
)の互いに向き合う羽根面(23、24)の半径面内に
あり、これら送風機羽根の少なくとも1つが補助羽根で
あることを特徴とする、特許請求の範囲第1項に記載の
送風装置。 7 スリット(7、18)が送風機囲い板(4)に結合
可能なキャップにより覆われることができることを特徴
とする、特許請求の範囲第1項または第2項または第5
項または第6項に記載の送風装置。
[Scope of Claims] 1. A blower impeller is supported by an internal combustion engine via a blower blade axle, a belt pulley for a drive belt is provided on the blower impeller shaft, and the blower impeller has an surround surrounding the outer end of the blower blade. In those equipped with a blower shroud, the blower shroud (4) inserts the belt (6) and connects the blower impeller (
1) Connect the belt part on the end face without the shaft to the blower shroud (
4) A blower device in a radiator for a water-cooled internal combustion engine, characterized in that it has at least one axially extending slit (7, 18) for displacing the air beyond. 2 Blower blades (3) with two adjacent slits (7)
The shrouding plate pieces (9, 10) on both sides of the slit (7), which are provided in the area of the fan shroud (4) located between The blower device according to claim 1, wherein the blower device is held. 3. The blower device according to claim 2, characterized in that the struts are constructed as auxiliary vanes (11, 12). 4. The blower device according to claim 2, characterized in that one support is formed by a blower blade (3) and the other support is formed by an auxiliary blade (11 or 12). 5 A slit (7) is provided in the shroud part (13) of the blower shroud (4) extending in the radial extension of the blower blade (3), allowing it to pass through the cutout (14) in the blower blade (3). 2. A blower device as claimed in claim 1, characterized in that it continues in the area of the blower boss (2). 6 A slit (18) is formed according to the axial course of the contour of the blower blade (19, 20), and both longitudinal edges (21, 22) of this slit are arranged along the axial direction of the contour of the blower blade (19, 20).
2. A blower device according to claim 1, characterized in that the blower blades are in the radial plane of mutually facing blade surfaces (23, 24) of the blower blades, at least one of which is an auxiliary blade. 7. Claims 1 or 2 or 5, characterized in that the slits (7, 18) can be covered by a cap connectable to the blower shroud (4).
The blower device according to item 6 or item 6.
JP60181956A 1984-08-30 1985-08-21 Air blower in radiator for water-cooled internal combustion engine Granted JPS6161909A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3431801A DE3431801C1 (en) 1984-08-30 1984-08-30 Air conveying device on a cooler for water-cooled internal combustion engine
DE3431801.1 1984-08-30

Publications (2)

Publication Number Publication Date
JPS6161909A true JPS6161909A (en) 1986-03-29
JPH0240853B2 JPH0240853B2 (en) 1990-09-13

Family

ID=6244214

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60181956A Granted JPS6161909A (en) 1984-08-30 1985-08-21 Air blower in radiator for water-cooled internal combustion engine

Country Status (7)

Country Link
US (1) US4655686A (en)
JP (1) JPS6161909A (en)
DE (1) DE3431801C1 (en)
FR (1) FR2569769B1 (en)
GB (1) GB2166807B (en)
IT (1) IT1182828B (en)
SE (1) SE458464B (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3832026A1 (en) * 1988-09-21 1990-03-22 Bosch Gmbh Robert FAN WHEEL
US6318067B1 (en) * 2000-01-14 2001-11-20 Michael M. Marquard Internal combustion engine with balanced rotary combustion chamber separate from reciprocating power cylinder
DE102004034813B4 (en) * 2004-07-19 2012-09-06 Man Truck & Bus Ag Noise-optimized jacket fan

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Publication number Priority date Publication date Assignee Title
GB190109478A (en) * 1901-05-07 1901-10-12 George Henry Cove Improvements relating to Screw Propellers.
US1209863A (en) * 1912-11-06 1916-12-26 Packard Motor Car Co Motor-vehicle.
US1203984A (en) * 1915-06-03 1916-11-07 Lyle D Corey Fan attachment for sewing-machines.
US1292830A (en) * 1916-02-18 1919-01-28 Packard Motor Car Co Cooling-fan.
US1291199A (en) * 1917-05-28 1919-01-14 Gen Motors Corp Accessory-drive for motor-vehicles.
US1278396A (en) * 1917-05-31 1918-09-10 Carl E W Speiser Automobile-radiator-cooling means.
FR569801A (en) * 1922-11-03 1924-04-18 Gill Propeller Company Ltd Improvements to propellers or equivalent components
US1873379A (en) * 1929-06-05 1932-08-23 Jr Herman C Frentzel Engine heating and cooling system
FR730955A (en) * 1931-02-17 1932-08-26 Allmanna Sevenska Elek Ska Akt Method and device for the manufacture of impellers for radial turbines
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US2823937A (en) * 1955-09-28 1958-02-18 Barre Leo L La V-belt pulley
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GB833938A (en) * 1957-04-01 1960-05-04 Caterpillar Tractor Co Self-cleaning fan guard
US3794001A (en) * 1973-03-02 1974-02-26 Ford Motor Co Variable tip clearance engine cooling fan shroud
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JPS5838319A (en) * 1981-08-31 1983-03-05 Nissan Motor Co Ltd Fan shroud

Also Published As

Publication number Publication date
IT1182828B (en) 1987-10-05
GB8521370D0 (en) 1985-10-02
JPH0240853B2 (en) 1990-09-13
SE458464B (en) 1989-04-03
GB2166807B (en) 1988-08-10
SE8504013L (en) 1986-03-01
SE8504013D0 (en) 1985-08-28
FR2569769B1 (en) 1988-07-08
US4655686A (en) 1987-04-07
DE3431801C1 (en) 1985-10-17
GB2166807A (en) 1986-05-14
FR2569769A1 (en) 1986-03-07
IT8548481A0 (en) 1985-08-20

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